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热等静压温度对第三代单晶高温合金DD10组织的影响 被引量:8

Effect of Hot Isostatic Pressing Temperature on the Microstructure of a Third Generation Single Crystal Superalloy DD10
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摘要 采用OM,SEM以及EPMA等手段对比研究了不同热等静压温度对第三代单晶高温合金DD10组织的影响。结果表明:在150MPa压力条件下,1290℃热等静压即可使第三代单晶高温合金DD10中的显微疏松完全闭合;随热等静压温度的升高,共晶体积分数逐渐减少,热等静压温度达到1310℃及以上温度,共晶完全溶于基体。在1340℃/150MPa热等静压后,合金中出现局部初熔。热等静压后DD10单晶高温合金的γ′相立方度提高,不同热等静压温度对γ′相的形貌影响基本相同。热等静压降低了DD10单晶高温合金的枝晶偏析,并且热等静压温度越高,枝晶偏析改善越明显。 The effects of different hot isostatic pressing temperatures on the microstructures of the third generation single crystal superalloy DD10 were investigated by using optical microscope (OM), scanning electron microscope (SEM) and electron microprobe analyzer (EPMA). The results show that the hot isostatic pressing temperature 1290℃ was enough for the mieroporosity of DD10 to be eliminated completely at 150MPa; the volume fraction of euteetic was decreased markedly with the increase of the hot isostatic pressing temperature. The euteetie disappeared with hot isostatic pressing of 1310℃ or above, and there were internal incipient melting after hot isostatic pressing at 1340℃/ 150MPa. Meanwhile, the hot isostatic pressing process with different temperatures also resulted in more uniform morphology of γ precipitates to the same extent. The dendritic segregation was homogenized gradually because of increasing of the hot isostatic pressing temperature.
出处 《材料工程》 EI CAS CSCD 北大核心 2013年第6期1-4,24,共5页 Journal of Materials Engineering
关键词 DD10 热等静压 温度 显微疏松 共晶 枝晶偏析 DD10 hot isostatic pressing temperature microporosity eutectic dendritic segregaton
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参考文献16

  • 1胡壮麒,刘丽荣,金涛,孙晓峰.镍基单晶高温合金的发展[J].航空发动机,2005,31(3):1-7. 被引量:237
  • 2陈荣章.单晶高温合金发展现状[J].材料工程,1995,23(8):3-12. 被引量:110
  • 3REED R C.The superalloys:Fundamentals and applications[M].Cambridge,UK:Cambridge University Press,2006.
  • 4石琳.涡轮叶片用单晶高温合金的发展[J].航空工程与维修,2000(6):35-37. 被引量:5
  • 5曹腊梅,杨曦桥,薛明,蔡启舟.定向凝固过程中温度参数对含Re镍基单晶高温合金铸态组织的影响[J].材料工程,2012,40(10):8-11. 被引量:8
  • 6东华.第三代单晶高温合金[J].航空制造工程,1995(12):9-11. 被引量:3
  • 7ERICKSON G L.The development of CMSX-10,a third generation SX casting superalloy.The Second Pacific Rim International conference on Advanced Materials and Processing.Kyongju,Korea:TMS,1995.18-22.
  • 8BURGEL R,PORTELLA P D,PREUHS J.Recrystallization in single crystals of nickel base superalloys.POLLOCK T M,KISSINGER R D,BOWMAN R R,et al.Superalloy 2000.Warrendale,PA,USA:TMS,2000.229-238.
  • 9CHANG J C,CHOI C,KIM J C,et al.Development of microstructure and mechanical properties of a Ni-base single-crystal superalloy by hot-isostatic pressing[J].Journal of Materials Engineering and Performance,2003,12(4):420-425.
  • 10FRITZEMEIER L G.The influence high thermal gradient casting,hot isostatic pressing and alternate heat treatment on the structure and properties of a single crystal nickel base superalloy.REICHMAN S,DUHL D N,MAURER G,et al.Superalloys 1988.Champion,PA:TMS,1988.305-314.

二级参考文献57

  • 1李乐平,赵宏宇,陶午沙.基于VRML标准的大场景三维地形数据浏览系统[J].装备指挥技术学院学报,2000,11(5):11-17. 被引量:2
  • 2孔祥鑫.第四代战斗机及其动力装置[J].航空科学技术,1994(5):21-23. 被引量:9
  • 3陈荣章.单晶高温合金发展现状[J].材料工程,1995,23(8):3-12. 被引量:110
  • 4胡壮麒,刘丽荣,金涛,孙晓峰.镍基单晶高温合金的发展[J].航空发动机,2005,31(3):1-7. 被引量:237
  • 5[2]MICHAEL WOULDS,HOWARD BENSON. Development of a conventional fine grain casting process [C]. Superalloy 1984, A Publication of The Metallurgical Society of AIME,7-11.
  • 6[3]ZHENG Y,HAN Y.Influencing factors of stress rupture at 750℃ temperature for cast nickel base superalloy K403[A].In: SAKUMA T,YAGI K,ed. Creep and Fracture of Engineering Materials and Structure [C].Switzerland:trans Tech Publications Ltd,1999,561-568.
  • 7Pollock T M, Tin S. JPropul Power[J], 2006, 22(2): 361.
  • 8Feng Q, Nandy T K, Tin S et al. Aeta Mater[J], 2003, 51(1): 269.
  • 9Sato A, Harada H, Yokokawa T et aL Scripta Mater[J], 2006, 54(9): 1679.
  • 10Tin S, Zhang L, Hobbs R et al. In: Reed R C et al eds. Superalloys 2008[C]. Champion, PA: TMS, 2008:81.

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